FIXTURE FOR RESTRAINING A TURBINE WHEEL
A fixture for restraining a wheel of a turbomachine has a dovetail section adapted for insertion into a dovetail slot of the wheel. A mounting section is located adjacent to, or formed integrally with, the dovetail section. At least one coupling ring is attached to the mounting section, and the coupling ring is adapted to be secured to a stationary anchoring point via a restraint. The stationary anchoring point includes at least one counterbore assembly having a coupling ring attached thereto. The counterbore assembly is adapted to be secured to a stationary structure. The stationary structure may be a shell, a flange or a casing of the turbomachine.
Latest General Electric Patents:
The apparatus described herein relates generally to turbomachinery and, more specifically, to a fixture for restraining a turbine wheel during a blade removal or installation procedure.
Turbomachines need regular maintenance to keep up with the cycle type, in which some cases are continuous (6,000 hours/year or more). During an inspection maintenance outage, the blades in the turbine section of the turbomachine may need to be replaced. The top half of the turbine case is removed, and technicians will restrain the rotor from rolling and begin to remove or replace the turbine blades. To restrain the rotor, technicians have tied a strap around a blade and then attached it to somewhere in the turbine compartment. This known method could result in near miss or incidents which involve the rotor rolling due to a broken strap, as well as damage caused to the blade. The known method that uses a strap presents a risk of injury, safety concerns, as well as requiring possible replacement parts due to hardware damage.
BRIEF DESCRIPTION OF THE INVENTIONIn an aspect of the present invention, a fixture for restraining a wheel of a turbomachine has a dovetail section adapted for insertion into a dovetail slot of the wheel. A mounting section is located adjacent to, or formed integrally with, the dovetail section. At least one coupling ring is attached to the mounting section, and the at least one coupling ring is adapted to be secured to a stationary anchoring point via a restraint.
In another aspect of the present invention, a fixture for restraining a wheel of a turbomachine includes a dovetail section adapted for insertion into a dovetail slot of the wheel. The dovetail section has a dovetail shaped profile or fir tree shaped profile adapted to interlock with corresponding notches or recesses in the dovetail slot of the wheel. The dovetail section has an aft end and a forward end, and both the aft end and the forward end have a threaded hole adapted for securing a fastener. A mounting section is located adjacent to, or formed integrally with, the dovetail section. The mounting section has at least one threaded hole adapted for attaching a coupling ring to the mounting section. A coupling fastener and a washer secures the coupling ring to the mounting section via the at least one threaded hole. The coupling ring is attached to the mounting section, and the at least one coupling ring is adapted to be secured to a stationary anchoring point via a restraint.
In yet another aspect of the present invention, a method for restraining a wheel of a turbomachine is provided. The method includes a step of inserting a fixture into a dovetail slot in the wheel. The fixture has dovetail section adapted for insertion into the dovetail slot, and a mounting section located adjacent to, or formed integrally with, the dovetail section. The mounting section is adapted to connect to at least one coupling ring. The inserting step may also include placing a washer over a fastener, and inserting the fastener into a threaded hole in the dovetail section, wherein the washer is adapted to extend over an axial face of the dovetail slot. In addition, the inserting step may include attaching the at least one coupling ring to the mounting section. An attaching step attaches at least one counterbore assembly to a stationary structure, and a connecting step connects a restraint to the at least one coupling ring and the at least one counterbore assembly. The connecting step may also include attaching a come-along or ratcheting mechanism having a strap, chain or cable to both the at least one coupling ring and the at least one counterbore assembly, and tightening the come-along or ratcheting mechanism to restrain the wheel. The stationary structure may be a shell, a flange or a casing of the turbomachine. The dovetail section may have a straight profile adapted for use with a straight dovetail slot, or an angled profile adapted for use with an angled dovetail slot, or a curved profile adapted for use with a curved dovetail slot.
One or more specific aspects/embodiments of the present invention will be described below. In an effort to provide a concise description of these aspects/embodiments, all features of an actual implementation may not be described in the specification. It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions must be made to achieve the developers' specific goals, such as compliance with machine-related, system-related and business-related constraints, which may vary from one implementation to another. Moreover, it should be appreciated that such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure.
When introducing elements of various embodiments of the present invention, the articles “a,” “an,” and “the” are intended to mean that there are one or more of the elements. The terms “comprising,” “including,” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements. Any examples of operating parameters and/or environmental conditions are not exclusive of other parameters/conditions of the disclosed embodiments. Additionally, it should be understood that references to “one embodiment”, “one aspect” or “an embodiment” or “an aspect” of the present invention are not intended to be interpreted as excluding the existence of additional embodiments or aspects that also incorporate the recited features.
Referring to
The combustor assembly 14 uses a combustible liquid and/or gas fuel, such as a natural gas or a hydrogen rich synthetic gas, to run the gas turbine 10. The combustor assembly 14 includes a combustor chamber 20 that is in fluid communication with a fuel pre-mixer 22 that is in fluid communication with an airflow 24 and a fuel source 26. The fuel pre-mixer 22 creates an air-fuel mixture, and discharges the air-fuel mixture into the combustor chamber 20, thereby causing a combustion that creates a hot pressurized exhaust gas. The combustor chamber 20 directs the hot pressurized gas through a transition piece into the turbine 16, causing rotation of the turbine 16. Rotation of the turbine 16 causes the shaft 18 to rotate, thereby compressing air as it flows into the compressor 12. The turbine section 16 has multiple rotatable wheels 17 on which a plurality of blades are mounted. In this example, three stages of turbine wheels 17 are shown, and each wheel would be paired with a stator vane stage (not shown). In general, turbomachines include, compressors, gas turbines and steam turbines.
In use, the coupling ring 340 is secured to a stationary anchoring point via a restraint. To lock the fixture into the dovetail slot 201, stops 350, 360, 450 are used on axial ends or axial faces thereof. The fixture 210 has a forward axial face (or end) 370 and an aft axial face (or end) 371. The stop 350 is configured as a T-shaped stop and the top of the “T” extends past the outline of the dovetail slot 201. In this manner, the stop 350 rests against a forward axial face of wheel 17 and prevents axial movement of the fixture. The stop 350 is attached to the dovetail section 320 by means of a fastener 352, such as a shoulder screw or bolt. The aft axial face 371 has a fastener 362 and washer 360 that function as a stop. The washer 360 is sized so that it overlaps the dovetail slot boundary, and in so doing prevent axial movement of the fixture. When both stops 350, 360 are installed, the dovetail section 320 is locked in the dovetail slot 201, and the fixture will not slide out of the slot 201.
In step 1120, at least one counterbore assembly 810 is attached to a stationary structure 820. In step 1130 a restraint 830 is connected to the coupling ring 340 and the at least one counterbore assembly 810. Steps 1120 and 1130 may be repeated until the desired number of restraints are installed. Connecting step 1130 may also include attaching a come-along 1010 having a strap, chain 830 or cable to both the coupling ring 340 and the counterbore assembly 810 or other coupling ring 812 located on the stationary support. In step 1140, the restraints are tightened to restrain or prevent the wheel 17 from rotating.
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.
Claims
1. A fixture for restraining a wheel of a turbomachine, the fixture comprising:
- a dovetail section adapted for insertion into a dovetail slot of the wheel;
- a mounting section located adjacent to, or formed integrally with, the dovetail section;
- at least one coupling ring attached to the mounting section; and
- wherein the at least one coupling ring is adapted to be secured to a stationary anchoring point via a restraint.
2. The fixture of claim 2, the stationary anchoring point further comprising:
- at least one counterbore assembly having a coupling ring attached thereto, the at least one counterbore assembly adapted to be secured to a stationary structure.
3. The fixture of claim 2, wherein the stationary structure is at least one of:
- a shell, a flange or a casing of the turbomachine.
4. The fixture of claim 1, the dovetail section having a dovetail shaped or fir tree shaped profile adapted to interlock with corresponding notches or recesses in the dovetail slot of the wheel.
5. The fixture of claim 4, the fixture further comprising an aft end and a forward end, both the aft end and the forward end having a threaded hole adapted for securing a fastener.
6. The fixture of claim 5, further comprising the fastener and a washer secured by the threaded hole, and a stop located on an opposing end of the fixture, the washer and the stop adapted to lock the dovetail section to the dovetail slot.
7. The fixture of claim 5, at least one of the aft end or forward end having:
- a T-shaped stop or a rectangular shaped stop.
8. The fixture of claim 1, the dovetail section having one of:
- a straight profile adapted for use with a straight dovetail slot, or
- an angled profile adapted for use with an angled dovetail slot, or
- a curved profile adapted for use with a curved dovetail slot.
9. The fixture of claim 1, the mounting section further comprising:
- at least one threaded hole adapted for attaching the coupling ring to the mounting section, and wherein a fastener secures the coupling ring to the mounting section via the at least one threaded hole.
10. The fixture of claim 1, further comprising:
- a first coupling ring attached to an aft end of the mounting section, and
- a second coupling ring attached to a forward end of the mounting section.
11. The fixture of claim 1, further comprising:
- a first coupling ring and a second coupling ring attached to the mounting section.
12. A fixture for restraining a wheel of a turbomachine, the fixture comprising:
- a dovetail section adapted for insertion into a dovetail slot of the wheel, the dovetail section having a dovetail shaped profile or fir tree shaped profile adapted to interlock with corresponding notches or recesses in the dovetail slot of the wheel, the dovetail section having an aft end and a forward end, both the aft end and the forward end having a threaded hole adapted for securing a fastener;
- a mounting section located adjacent to, or formed integrally with, the dovetail section, the mounting section having at least one threaded hole adapted for attaching a coupling ring to the mounting section, and wherein a coupling fastener secures the coupling ring to the mounting section via the at least one threaded hole;
- the coupling ring attached to the mounting section; and
- wherein the at least one coupling ring is adapted to be secured to a stationary anchoring point via a restraint.
13. The fixture of claim 12, the stationary anchoring point further comprising:
- at least one counterbore assembly having a coupling ring attached thereto, the at least one counterbore assembly adapted to be secured to a stationary structure, and the stationary structure being a shell, a flange or a casing of the turbomachine.
14. The fixture of claim 13, the dovetail section having one of:
- a straight profile adapted for use with a straight dovetail slot, or
- an angled profile adapted for use with an angled dovetail slot, or
- a curved profile adapted for use with a curved dovetail slot.
15. The fixture of claim 14, further comprising:
- a first coupling ring attached to an aft axial face of the mounting section, and
- a second coupling ring attached to a forward axial face of the mounting section.
16. A method for restraining a wheel of a turbomachine, the method comprising:
- inserting a fixture into a dovetail slot in the wheel, the fixture comprising: a dovetail section adapted for insertion into the dovetail slot; a mounting section located adjacent to, or formed integrally with, the dovetail section, the mounting section adapted to connect to at least one coupling ring;
- attaching at least one counterbore assembly to a stationary structure;
- connecting a restraint to the at least one coupling ring and the at least one counterbore assembly.
17. The method of claim 16, the stationary structure comprising at least one of:
- a shell, a flange or a casing of the turbomachine.
18. The method of claim 17, the inserting a fixture step further comprising:
- placing a washer or a stop over a fastener;
- inserting the fastener into a threaded hole in the dovetail section; and
- wherein the washer of the stop is adapted to extend over an axial face of the dovetail slot.
19. The method of claim 18, the inserting a fixture step further comprising:
- attaching the at least one coupling ring to the mounting section.
20. The method of claim 18, the connecting step further comprising:
- attaching a come-along having a strap, chain or cable to both the at least one coupling ring and the at least one counterbore assembly, and tightening the come-along to restrain the wheel.
Type: Application
Filed: Sep 27, 2016
Publication Date: Mar 29, 2018
Patent Grant number: 10024164
Applicant: General Electric Company (Schenectady, NY)
Inventors: Maxwell Evan Miller (Simpsonville, SC), Jason Matthew Clark (Maryville, TN), Sandra Beverly Kolvick (Simpsonville, SC)
Application Number: 15/277,327